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Near-hover control of a helicopter with a hanging loadPiloting a helicopter with a hanging load is a difficult task, especially when the mass of the load is a significant fraction of the mass of the vehicle and there are gusty winds. An autopilot logic is proposed here for controlling the helicopter in this configuration and for precision hover. It is proposed that the vehicle position be measured using a lightweight cable from the helicopter to a point on the ground near the desired hover point. Simulation with one version of S-61 Sikorsky helicopter shows satisfactory controller performance under both design conditions and for parameter changes from one mission to another. Assuming noise-free measurements for feedback is found to be far too optimistic in predicting performance, the sensor/estimator design is a key element in the controller.
Document ID
19760047895
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gupta, N. K.
(Systems Control, Inc. Palo Alto, Calif., United States)
Bryson, A. E., Jr.
(Stanford University Stanford, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: Journal of Aircraft
Volume: 13
Subject Category
Aircraft Stability And Control
Accession Number
76A30861
Funding Number(s)
CONTRACT_GRANT: NAS2-5143
Distribution Limits
Public
Copyright
Other

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